TURBINE NOZZLE COMPLIANT JOINTS AND ADDITIVE METHODS OF MANUFACTURING THE SAME
A turbine nozzle formed of a superalloy, and including: an annular end-wall including a pocket, the pocket defining an inner surface within the annular end-wall; a vane, the vane including an airfoil portion and a boss portion, the vane extending from the pocket such that the boss portion is enclose...
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creator | Biery, Shannon Stimpson, Curtis Mader, Morgan Morris, Mark |
description | A turbine nozzle formed of a superalloy, and including: an annular end-wall including a pocket, the pocket defining an inner surface within the annular end-wall; a vane, the vane including an airfoil portion and a boss portion, the vane extending from the pocket such that the boss portion is enclosed within the pocket and the airfoil portion extends through the annular end-wall; and a seal within the pocket, the seal including one or more protrusions extending from the inner surface of the pocket and abutting the vane at one or both of the boss portion and the airfoil portion. |
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a vane, the vane including an airfoil portion and a boss portion, the vane extending from the pocket such that the boss portion is enclosed within the pocket and the airfoil portion extends through the annular end-wall; and a seal within the pocket, the seal including one or more protrusions extending from the inner surface of the pocket and abutting the vane at one or both of the boss portion and the airfoil portion.</description><language>eng</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2021</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210715&DB=EPODOC&CC=US&NR=2021215054A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210715&DB=EPODOC&CC=US&NR=2021215054A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Biery, Shannon</creatorcontrib><creatorcontrib>Stimpson, Curtis</creatorcontrib><creatorcontrib>Mader, Morgan</creatorcontrib><creatorcontrib>Morris, Mark</creatorcontrib><title>TURBINE NOZZLE COMPLIANT JOINTS AND ADDITIVE METHODS OF MANUFACTURING THE SAME</title><description>A turbine nozzle formed of a superalloy, and including: an annular end-wall including a pocket, the pocket defining an inner surface within the annular end-wall; a vane, the vane including an airfoil portion and a boss portion, the vane extending from the pocket such that the boss portion is enclosed within the pocket and the airfoil portion extends through the annular end-wall; and a seal within the pocket, the seal including one or more protrusions extending from the inner surface of the pocket and abutting the vane at one or both of the boss portion and the airfoil portion.</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNy7EKwjAQgOEuDqK-w4Gz0FT7AGdysZHmIubSoUspEifRQn1_dPABnP7l-5cFS7oeHRNw6PuWQAd_aR2ywDk4lgjIBtAYJ64j8CRNMBGCBY-cLOrv7vgE0hBE9LQuFvfxMefNr6tia0l0s8vTa8jzNN7yM7-HFKuyUpWqy_qAav-f-gDiSi9v</recordid><startdate>20210715</startdate><enddate>20210715</enddate><creator>Biery, Shannon</creator><creator>Stimpson, Curtis</creator><creator>Mader, Morgan</creator><creator>Morris, Mark</creator><scope>EVB</scope></search><sort><creationdate>20210715</creationdate><title>TURBINE NOZZLE COMPLIANT JOINTS AND ADDITIVE METHODS OF MANUFACTURING THE SAME</title><author>Biery, Shannon ; Stimpson, Curtis ; Mader, Morgan ; Morris, Mark</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2021215054A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2021</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Biery, Shannon</creatorcontrib><creatorcontrib>Stimpson, Curtis</creatorcontrib><creatorcontrib>Mader, Morgan</creatorcontrib><creatorcontrib>Morris, Mark</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Biery, Shannon</au><au>Stimpson, Curtis</au><au>Mader, Morgan</au><au>Morris, Mark</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TURBINE NOZZLE COMPLIANT JOINTS AND ADDITIVE METHODS OF MANUFACTURING THE SAME</title><date>2021-07-15</date><risdate>2021</risdate><abstract>A turbine nozzle formed of a superalloy, and including: an annular end-wall including a pocket, the pocket defining an inner surface within the annular end-wall; a vane, the vane including an airfoil portion and a boss portion, the vane extending from the pocket such that the boss portion is enclosed within the pocket and the airfoil portion extends through the annular end-wall; and a seal within the pocket, the seal including one or more protrusions extending from the inner surface of the pocket and abutting the vane at one or both of the boss portion and the airfoil portion.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
title | TURBINE NOZZLE COMPLIANT JOINTS AND ADDITIVE METHODS OF MANUFACTURING THE SAME |
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